A Simulation Environment for Testing and Research of Neurally Augmented Fault Tolerant Control Laws Based on Non-Linear Dynamic Inversion
Author:
Affiliation:
1. West Virginia University
2. University of Perugia
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4913
Reference20 articles.
1. Fault tolerant flight control via adaptive neural network augmentation
2. Adaptive Autopilot Design for Guided Munitions
3. Augmentation of a non linear dynamic inversion scheme within the NASA IFCS F-15 WVU simulator
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